CA1202764A

CA1202764A - Fibre-reinforced metals

Info

Publication number: CA1202764A
Application number: CA000421051A
Authority: CA
Inventors: Stuart E. Booth; Andrew W. Clifford; Noel J. Parratt
Original assignee: UK Secretary of State for Defence
Current assignee: UK Secretary of State for Defence
Priority date: 1982-02-08
Filing date: 1983-02-07
Publication date: 1986-04-08
Also published as: WO1983002782A1; AU1227183A; DE3366357D1; AU555685B2; US4573517A; EP0100348B1; JPH0234271B2; EP0100348A1; GB2115327B; GB8302957D0; GB2115327A; JPS59500135A

Abstract

ABSTRACT
A fibre reinforced metal is made by introducing an array of fibres into a die, charging the die with molten metal by vacuum infiltration and then applying pressure by means of an inert gas to improve the penetration of the molten metal into the fibre array. Apparatus for producing a reinforced metal cylinder comprises a cylindrical former onto which a composite fibre of boron, silicon and carbon is wound.
The former forms an inner closure member for the die defining a cylindrical die cavity with an outer die body. A central cavity within the former is for insertion of a heating element to facilitate the flow of metal through the cavity. The die cavity is evacuated via conduit and molten metal is then drawn into the cavity via the passage.
After charging the die with molten metal the conduit is connected to a source of high pressure nitrogen. The die is then cooled while maintaining the pressure in the die cavity making use of a cooling stalk which replaced the heating element inside the spool.

Description

PROC~SS AND APPARATUS FOR ~IBRE REINFORCED METALS

The invention relates to the manufacture of composite materials comprising a metal matrix incorporating a reinforcing material, particularly elongated single crystal fibres of re-fractory materials.
UK Patent No 1334358 describes the manufacture of metal composites by processes involving the application of a defined pressure programme to an admixture of the molten metal and particulate reinforcing meterial in a mould. By subsequent extrusion of the cast composite billet it is possible to align some of the reinforcing fibres in the direct;on of the extrusion, resulting in an improvement of the strength and stiffness of the composite as compared with the unreinforced metal. However, because of the difficulty experienced in obtaining high concentrations of fibre and the breakage of fibres during the extrusion process the strength and stiffness of the composite were considerably less than might have been expected.
VK Patent No 1359554 disclosed a method for improving the strength and stiffness of composite materials by providing a predetermined pattern of reinforcing fibre in a mould and then applying pressure to a charge of molten metal to force it through the fibres to give a composite. In practice it had been found that it was extremely difficult to force the molton metal to penetrate the fibres without breaking them. The invention sought to overcome this problem by separating the fibres such that there existed a maximum penetration distance through the fibres commensurate with the flow characteristics of the metal.
Both prior art processes described above adopted mechanical pressure applied directly by a piston to a charge of molten metal to promote penetration by the metal into the array of fibres.
However, because of losses in the system the nominal pressure applied was found to be greater than the pressure applied to the liquid metal inside the mould cavity~
It is an ob;ect of the present invention to improve penetration of the fibres by molten metal and to reduce the ` i~t ~

pressure losses involved when pressurizing the liquid metal.
This will improve the properties of a metal composite casting and allow thinner die components to be used.
The invention provides a process for forming a composité
material comprising a metal matrix incorporating a non-metallic fibrous reinforcement material including the step of providing in a mould chamber at least one layer of the fibrous reinforcement material, characterised in that there are the further successive steps of: evacuating the mould chamber; heating the mould chamber and fibrous material to a temperature above the solidus temperature of the metal; sucking molten metal up into the mould chamber substantially under the action of the partial pressure in the mould chamber; applying pressure to the contents of the mould chamber by means of (a) an inert compressed gas so as to force moulten metal to surround substantially all of the fibres of the array; and (b) removing the source of heat.
Preferably the molten metal is maintained at a constant temperature above the metal liquidus to promote flow penetration of the metal between the fibres. The temperature of the molten metal may be controlled by providing a heating jacket which surrounds the die. In a preferred method for charging the die with molten metal the process includes the further steps of connecting the mould chamber by a conduit to an evacuated reservoir to reduce the gas pressure in the mould chamber prior to opening a valve in another conduit connecting a crucible of molten metal to the die such that molten metal is drawn from the crucible through the conduit into the die. Advantageously the crucible and die are both surrounded by heating jackets. Where the metal used is an aluminum alloy the temperatures of the die and molten metal are maintained above the aluminum alloy liquidus temperature throughout the steps of filling the die and pressuring the molten metal. Prior to filling the die with the molten metal it is desirable to degas the metal.
In an alternative method which does not require a liquid metal valve a liquid metal conduit is connected betw~en the mould cavity and air-tight furnace, substantially at the base thereof, the mould cavity being evacuated via the conduit and the furnace, 1~27~

the furnace then being connected to a gas at low pressure, as for example atmospheric pressure, which forces molten metal to flow to the mould cavity an~ finally the gas being pressurized to improve the flow of molten metal into the array of reinforcing fibre. The gas may be air or an inert gas where it is desired to re-use surplus metal.
In one form suitable for producing composite metal tubes, the reinforcing material comprises a fibre which is wound around a cylindrical former to form a cylindrical fibre layer. In order to promote the flow of molten metal around the fibres in the layer the former is preferably provided with longitudinal grooves in its outer surface such that the molten metal can flow through the grooves and penetrate the fibre layer radially from the inner as well as the outer surface.
Advantageously the die is cooled at a controlled rate to ensure directional solidification of the molten metal. Preferably the cooling is done by introducing coolant through the central axis of the former. In a preferred arrangement the former is at least partly hollow such that a cooling stalk can be inserted into the Eormer. The cooling stalk may be replaced by a heating element for raising the die temperature prior to the introduction of the molten metal so as to maintain the temperature of the molten metal.
In order to minimise the thermal stresses occuring during cooling of the former the die is preferably arranged such that it includes at least one seal capable of permitting relative movement between the former and the die. Advantageously the said seal is at the upper end of the die, the charge of molten metal being limited such that molten metal does not contact said seal.
Preferably the gas in contact with the metal is inert.
In order that these and other features may be appreciated embodiments of the invention will now be described by way of example only with reference to the following drawings of which:
Figure 1 is a cross sectional view of a die for producing a composite metal cylinderi Figure 2 is a cross sectional view taken through the heating .~

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jackets surrounding the die and a crucible for melting the metal;
Figure 3 is a partial cross sectional view of the surface of the former shown in Figure 1.
Figure 4 is a part-sectional view of a modification of the apparatus of Figures I and 2; and Figure 5 is a sectional view of an alternative arrangement of the Figure 4 modification.
Figure 1 shows the die l which has been devised for the making of fibre-reinforced metal tubes. The materials selected for the tubes are Borsic fibres, composed of boron, silicon and carbon, and aluminum alloy.
A Borsic fibre is wound around a steel former 2 to form a cylindrical fibre array 3. The former is then inserted into the die l. The die 1 is formed by a hollow cylindrical body 4 in which are bolted end places 5 and 6. Molten aluminum alloy is introduced into the die 1 through the opening 7 in the lower portion of the cylindrical body 4 and is drawn up through a cylindrical space 8 surrounding the former 2 and the fibre array 3 until the fibre array is entirely covered by the molten metal. During this process it is necessary to maintain the temperature of the die such that the molten metal flows freely. Once the required charge of molten metal has been introduced into the die the molten metal is pressurised by a compressed inert gas so as to force the molten metal to flow through the fibre array 3 to form an intimate metal matrix linking the array.
The die is charged with molten metal as can be seen with further reference to Figure 2. Aluminum alloy is first melted and is then degassed. The molten metal is then transferred to a crucible 9. A tube 10 for introducing the molten metal into the die is inserted into the crucible and is connected to the opening 7 in the die 1 by a valve 11. The die 1 and crucible 9 are surrounded by heating jackets 12 and 13 to maintain the temperature of the aluminum alloy at 650C to 700~C. Heating elements 14 are inserted through the heating jacket 12 and the upper end plate 6 into the hollow interior 15 of the former 2 to maintain uniformity of temperature within the die. The space 8 :~;
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within the die I is evacuated with the value 11 in the closed position by connecting a conduit 16 which passes through the die top plate to a reservoir connected to a vacuum pump. The die is charged by opening the valve 11 to draw metal up into the die by virtue of the difference between the pressure in ~he mould chamber and atmospheric pressure acting on the metal in the cr~cible. The valve 11 is provided with two flow rate settings. The die is Eilled with the value fully open until the metal just covers the fibre array and then the flow is adjusted to a slower rate until the metal level reaches a position just below the seals 17 and 18 between the top plate 6 and respectively the former 2 and the body 4 of the die. The use of a controlled slow fill to the final level ensures that molten metal does not contact the die seals 17 and 18. A valve made by Flexitallic (Trade Mark) is used fitted with special seals which are stable up to 900C.
Two probes (not shown) are provided at appropriate heights in the wall of the body of the die to respectively determine the change from the initial metal flow rate to the final metal flow rate and then the valve closure.
The conduit 16 is connected to the vacuum reservoir via a metal tube 19, a flexible hose (not shown) and a ~hree way valve (not shown). After charging the die with molten metal the three-way valve is rese~ to connect to the die a gas bottle containing inert gas such as argon at a pressure of lS N/mm2. The gas pressure is applied to the molten metal to improve the penetration of the metal between the fibre windings such that the ~orsic fibre becomes entirely embedded within the molten metal. In order to further improve the metal penetration into the fibre array the outer surface of the former 2 is provided with longitudinal grooves 20 as can be seen in Figure 3. Under the influence of the partial vacuum during the charging of the die, molten metal flows up through the grooves 20 within the fibre array as well as through the annualar space 8 surrounding the fibre array. On pressurising the die molten metal is then able to penetrate the fibre array from radially inside as well as from outside the array.

'7~4 After pressurising the die cavity the hea~in~ elements 14 are removed fro~ within the interior 15 of the former 2 and a cooling stalk is inserted. Air is passed ~hrough the cooling stalk while the temperature of the die is monitored. By varying the flow rate and/or the temperature of the cooling gas the molten metal is cooled at a controlled rate ensuring directional solidification by virtue of the axial cooling of the former. Once the metal has solidified the gas pressure is removed and the heating jackets are removed to allow the casting and the die to cool.
Cooling of the former may alternatively be done by passing water through the cooling stalk. Stress within the die arises principally as a result of differential thermal contraction during the forced cooling of the former. This stress ;s minimized according to the design shown in Figure 1 by concentrating thermal movement in the region of the seal 17 between the former and the top end place 6 of the die. Thus an expansion space 21 is provided between the top of the former 2 and the top end plate 6. The seal 17 must therefore be capable of maintaining integrity during expansion and contraction of the former and to be effective at high temperatures. Since the metal level is kept below the level of the seal this requirement is less stringent. A seal known as Helico flex is used. This makes use of a spring with a metal facing so as to be capable of retaining gas pressure within the die during the longitudinal and radial contraction of the former due to the forced cooling. The seal 22 at the base of the die is made by a conventional spiral-wound stainless steel-asbestos type of seal such as the Flexitallic seal. Thus by providing efficient seals between the former and the die and adapting the seals to be capable of accepting any thermal expansion movement of the former, pressure losses are minimised and the pressure exerted on the molten metal is substantially equal to the nominal applied pressure.
The apparatus thus far described for carrying out the process of the invention utilises a value in the liquid metal conduit. Alternative arrangements are shown in Figures 4 and 5 which obviate the necessity for a liquid metal valve and thus avoid the consequent sealing problems.

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Figure 4 illustrates a die incorporating a cylindrical former for the reinforcing fibre as shown in Figure 1. In this embodiment however there is no hole through the top end-plate 6 of the die for evacuation and pressurisation of the mould cavity. In addition the liquid metal valve 11 indicated in Figure 2 is dispensed with.
Connected directly to the outer wall 23 of the die is a furnace 24 the interior of which is connected to the mould cavity by means of the liquid metal conduit or opening 7. A pipe 25 is provided within the furnace having one open end near the bottom of the furnace and the other end thereof connected to the liquid metal conduit or opening 7. A further conduit 26 is connected to an opening 27 near the top of a wall of the furnace 24.
As in the first embodiment a b~rsic reinforcing fibre is wound on a cylindrical former and the former connected within the ]5 outer die body forming a mould cavity between the die body and the former. The furnace 24 and the mold cavity are evacuated via the a charge of molten metal 28 ~as shown), or a melting furnace containing solid metal. In both cases air from the mould cavity is evacuated via the pipe 25 and in the former case bubbles up through the molten metal 28. When the temperature of the die and liquid metal are above the metal liquidus temperature the conduit 26 is connected to an inert gas at atmospheric pressure which thereby forces liquid metal to substantially fill the die cavity.
The inert gas is then pressurised, forcing the liquid metal to improve the penetration of the liquid metal into the Borsic fibre array.
Figure 5 is an alternative apparatus needing no liquid metal valve. Insulation material 29 for surrounding a heating element 30, a die 31 and a furnace 32 is shown partly removed for clarity.
A former 33 has a cylindrical upper portion 34 on which a continuous borsic fibre 35 is wound. The upper portion 34 has a hollow bore 36 extending approximately half way through the portion and being filled at its innermost end with insulating material 37. A circular flange 38 integrally formed with the upper portion 34 forms a closure member of the die when the former is inserted into a cylindrical outer die body 39. A circular sealing gasket 40 is provided in the lower end of the die body 40 to seal against the upper surface of the flange 38. A seal 41 is situated in a stepped recess provided at the upper end of the inner surface of the die body 39 to seal against the cylindrical outer surface of the upper portion 34 of the former.
Extending downwards from the circular flange 38 is a stalk 40.
An axial bore 41 through the stalk 40 is connected to a metal feed hole 42 which is bored diametrically through the upper portion 34 of the former. The furnace 32, which as before may be a holding furnace or a melting furnace, is provided at the upper end with a ~~ circular gasket 43 for sealing against the lower surface of the flange 38. A conduit 44 is provided through the upper wall of the furnace.
As in the Figure 4 arrangement a borsic fibre is wound on to the upper portion 34 of the former 33 and the former is then assembled within the outer die body 39 forming a die cavity 44.
The furnace 32 in then assembled with the die, the length of the stalk 40 being such its open end is near the bottom of the furnace. The furnace and die cavity are then evacuated via the conduit 44, the bore 41 and the metal feed hole 42. After evacuation and with the liquid metal temperature and die temperature above the metal liquidus temperature the conduit 44 is first connected to an inert gas at a low pressure to substantially fill the die cavity 45 with liquid metal and then the inert gas is pressurised to improve the liquid metal penetration into the reinforcing fibre array. Any gas remaining within the die chamber is compressed into a region around the upper die seal 41. After pressurising the die the upper insulation is removed and cooling air 46 is blown onto the upper surface of the die and into the hollow bore 36 within the former 33. The insulating material 37 ensures that cooling occurs through the cylindrical wall of the hollow bore 36 while inhibiting axial cooling of the former which might cause freezing of the liquid metal in the metal feed hole 42. Thus the charge of molten metal in the die cools from the top and further pressurised liquid t7~j~
_g _ metal is able to enter the die to fill any cavities which might arise due to differential contraction on cooling and freezing.
Materials investigated for construction of the die body and end-plates were mild steel, 18/8 type chromium-nickel stainless steels and nickel-base superalloys. Mi]d steel was rejected because its properties are inadequate at 650C. Nickel-base superalloys gave between 50%-100% improvement on yield strength and design strength but castings were up to ten times more expensive. The material chosen was 18% Cr - 9% Ni - 22% Mo to ASTM A351 CF8M. Preferably the die body and end plates are centrifugally cast. Testing has shown that after various heat treatments the tensile properties of Borsic fibres are unimpaired.
The bendability of the fibres was in fact found to improve and thus there is no serious constraing on the time which can be allowed to heat up the die including the fibre array to the operating temperature until it can be evacuated and filled with molten metal.
For small die castings it rnay prove advantageous to use a split die to facilitate separation of the casting from the die 20 components. For such castings the die structure may be simplified by dispensing with the axial cooling facility.
, Although the invention has been described with reference to the accompanying Figures it will be apparent to those skilled in the art that other modifications are possible. Thus the provision of longitudinal grooves on the former could be eliminated by ensuring that the density of fibres in the fibre array is sufficiently low and the gas pressure sufficiently high for molten metal to penetrate the array from one side only and to completely surround the fibres. It is further envisaged that the application of gas pressure in the formation of composite materials may be used to cast shapes other than the tube described.
A further improvement in the manufacture of a composite metal tube could be achieved by the use of fibre -tapes, woven fibres or bundles of fibres to lay on the former to reduce the time required to wind a single fibre on to the former. In order to minimise the undesirable effects of air leaking through seals '`~

into the mould cavity, an inert gas atmosphere could be provided around these seals.

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Claims

CLAIMS:

1. A process for forming a composite material comprising a metal matrix incorporating a non-metallic fibrous reinforcement material including the step of providing in a mould chamber at least one layer of the fibrous reinforcement material, characterised in that there are the further successive steps of: evacuating the mould chamber; heating the mould chamber and fibrous material to a temperature above the solidus temper-ature of the metal; sucking molten metal up into the mould chamber sub-stantially under the action of the partial pressure in the mould chamber;
applying pressure to the contents of the mould chamber by means of (a) an inert compressed gas so as to force molten metal to surround substan-tially all of the fibres of the array; and (b) removing the source of heat.

2. A process according to claim 1 wherein the temperatures of the die and molten metal are maintained above the liquidus temperature throughout the steps of filling the die and pressuring the molten metal.

3. A process according to claim 2 wherein the method for charging the die with molten metal includes the further steps of connecting the die by a conduit to an evacuated reservoir to reduce the gas pressure in the die prior to opening a valve in another conduit connecting a cruicible of molten metal to the die such that molten metal is drawn from the crucible through the conduit into the die.

4. A process according to claim 3 wherein the crucible and die are surrounded by heating jackets.

5. A process according to claim 4 including the step of cooling the die while applying pressure to the molten metal, the cooling being controlled to ensure directional solidification of the molten metal.

6. A process according to claim 5 wherein the metal is degassed prior to filling the die.

7. A process according the claim 6 wherein the metal is an aluminium alloy.

8. A process according to claim 7 wherein the fibre is composed of boron, carbon and silicon.

9. A process as claimed in claim 1 wherein a liquid metal conduit is connected between the die and an air-tight furnace substantially at the base thereof, including the further steps of evacuating the furnace to thereby evacuate the die via the metal conduit, connecting the furnace to a source of gas at a low pressure to thereby force molten metal to substantially fill the die, and finally pressurising the gas to thereby pressurise the molten metal in the die.

10. A process according to claim 9 wherein the temperatures of the die and molten metal are maintained above the liquidus temperature throughout the steps of filling the die and pressuring the molten metal.

11. A process according to claim 10 wherein the crucible and die are surrounded by heating jackets.

12. A process according to claim 11 including the step of cooling the die while applying pressure to the molten metal, the cooling being controlled to ensure directional solidification of the molten metal.

13. A process according to claim 12 wherein the metal is degassed prior to filling the die.

14. A process according to claim 13 wherein the metal is an aluminium alloy.

15. A process according to claim 14 wherein the fibre is composed of boron, carbon and silicon.